a * 14200 GPa; /= 1120 × 106 mm4]. If w=66 kN/m and P= 128 kN, determine:PAY, VA1.5 mBW3.5 mleet[VITCnumeratorΕΙde-itange snape [E2.5 mFigure Q.2Part A: The reactions at A, B, and D. Choose the reaction force at B as the redundant; therefore,the released beam is simply supported between A and D.a) Calculate the value of the deflection at point B due to uniformly distributed load win theformDUBNote: E/ will cancel out in further calculations.Enter the numerator in the answer box below in kNm³ to three decimal places. Assume thepositive direction of deflection in the positive direction of v axis.X Part B. The magnitude of the maximum bending stress in the beam.f) Find the maximum bending moment in the beam. Enter your answer in kNm to two decimalplaces.Answer:Checkg) Calculate the magnitude of the maximum bending stress in the beam. Enter your answer inMPa to two decimal places

The beam shown in Figure Q.2 consists of a W610 × 140 structural steel wide-flange shape [E = 200…

The beam SNOV Figure Q.Z 200 GPa; /= 1120 × 106 mm4]. If w= 66 kN/m and P= 128 kN, determine: X P AY, V 1.5 m B W 3.5 m 140 structural steet wide-ange shape [2- UB Note: E/will cancel out in further calculations. с Figure Q.2 Part A: The reactions at A, B, and D. Choose the reaction force at Bas the redundant; therefore, the released beam is simply supported between A and D. 2.5 m a) Calculate the value of the deflection at point B due to uniformly distributed load win the form numerator EI

The beam SNOV Figure Q.Z 200 GPa; /= 1120 × 106 mm4]. If w= 66 kN/m and P= 128 kN, determine: X P AY, V 1.5 m B W 3.5 m 140 structural steet wide-ange shape [2- UB Note: E/will cancel out in further calculations. с Figure Q.2 Part A: The reactions at A, B, and D. Choose the reaction force at Bas the redundant; therefore, the released beam is simply supported between A and D. 2.5 m a) Calculate the value of the deflection at point B due to uniformly distributed load win the form numerator EI

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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Concept explainers

Matrix Algebra for Structural analysis

Structural analysis is a process in which the effects of different loads and internal forces, acting on structures and their elements are determined. This method of analysis is effective in detecting the failure loads of the structural elements and the design can be altered before commencing the construction process, which ensures proper strength and safety of the structures.

Question

a * 14
200 GPa; /= 1120 × 106 mm4]. If w=66 kN/m and P= 128 kN, determine:
P
AY, V
A
1.5 m
B
W
3.5 m
leet
[VIT
C
numerator
ΕΙ
de-itange snape [E
2.5 m
Figure Q.2
Part A: The reactions at A, B, and D. Choose the reaction force at B as the redundant; therefore,
the released beam is simply supported between A and D.
a) Calculate the value of the deflection at point B due to uniformly distributed load win the
form
D
UB
Note: E/ will cancel out in further calculations.
Enter the numerator in the answer box below in kNm³ to three decimal places. Assume the
positive direction of deflection in the positive direction of v axis.
X

Part B. The magnitude of the maximum bending stress in the beam.
f) Find the maximum bending moment in the beam. Enter your answer in kNm to two decimal
places.
Answer:
Check
g) Calculate the magnitude of the maximum bending stress in the beam. Enter your answer in
MPa to two decimal places

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Step 1: Introducing given data

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Step 2: Taking reaction at B as redundant

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Step 3: Calculate vertical reaction at A for simply supported beam AD for udl & load

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Step 4: Using double integration method to calculate deflection at B due to udl w

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Step 5: Using double integration method to calculate deflection at B due to load P

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Step 6: Using double integration method to calculate deflection at B due to reaction By

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Step 7: Calculate reaction at B

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Step 8: Calculate max moment

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Step 9: Calculate max bending stress

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